View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55767U 26145.43080037 +.00000000 +00000-0 +10369-3 0 00008
2 55767 70.0001 31.1503 0002786 272.4658 87.6183 14.98341539 00
| Epoch (UTC): | 25 May 2026 10:20:21 |
| Eccentricity: | 0.0002786 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.1503° |
| argument of perigee: | 272.4658° |
| revolutions per day: | 14.98341539 |
| mean anomaly at epoch: | 87.6183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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